# Service difficulty reports: N679SA

A list on [N679SA](https://openairdocs.org/aircraft/N679SA.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 3 · 118 reports

- [SDR SWIA20250429008](https://openairdocs.org/sdr/SWIA20250429008.md): Warning Message · false activation · Apr 28, 2025 · N679SA · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE WARNING ON CLIMBOUT. GEAR UP MISTAKENLY DELAYED AND SELECTED UP ONCE AT 250KT. NOSE GEAR WOULDN€™T RETRACT. QRH FIXED ISSUE. (FLIGHT 4807 - FILED CLOSED)GEAR DISAGREE MESSAGE CAUSED BY OVERSPEED CONDITION OF THE GEAR. PERFORMED GEAR OVERSPEED I
- [SDR SWIA2025012712](https://openairdocs.org/sdr/SWIA2025012712.md): Door Sill · corroded · Dec 12, 2024 · N679SA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > UPON REMOVAL OF SERVICE DOOR SURROUND STRUCTURE LOWER SILL FOUND CORROSION ON LOWER STRUCTURE. (C-CHECK RO 1/26/2025) COMPLIED WITH REO 601R-53-21-3709 FOR REPAIR OF AREA. TASK CARD 51-900-1003-SKY COMPLETEDE, M-337 ATTACHED. CPCP CARD EMAILED MANUALL
- [SDR SWIA2020127005](https://openairdocs.org/sdr/SWIA2020127005.md): Door Sill · corroded · Dec 5, 2024 · N679SA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > WHILE WORKING SERVICE DOOR SURROUND STRUCTURE LWR SILL FOUND SERVICE DOOR AFT LOWER SILL TO BE CORRODED. (C-CHECK RO 1/26/2025) REMOVED AND REPLACED SERVICE DOOR SURROUND STRUCTURE LWR SILL P/N 601R38303-253 IAW CRJ200 SRM 51-42-02. TASK CARD 51-900-10
- [SDR SWIA202501270088](https://openairdocs.org/sdr/SWIA202501270088.md): Web · cracked · Nov 19, 2024 · N679SA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > WEB CRACKED AT THE ACCUMULATOR BRACKET F.S. 200 LBL 40. (C-CHECK RO 1/26/2025) REPAIRED CRACK AT THE ACCUMULATOR BRACKET IAW CRJ 200 SRM REO 601R53-11-081TASK CARD 51-900-1003-SKY COMPLETED. M-337 ATTACHED
- [SDR SWIA202501270087](https://openairdocs.org/sdr/SWIA202501270087.md): Structure · cracked · Nov 19, 2024 · N679SA · Cndair CL6002B19 · Fuselage Main, Structure
  > CRACK IN CENTER WING BOX FS 461.5 RBL 4. (C-CHECK RO 1/26/2025) COMPLIED WITH REO 601R-53-41-3272 FOR REPAIR OF AREA.TASK CARD 51-900-1003-SKY COMPLETED. M-337 ATTACHED
- [SDR SWIA20250127114](https://openairdocs.org/sdr/SWIA20250127114.md): Door Sill · corroded · Nov 14, 2024 · N679SA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR SURROUND STRUCTURE LWR SILL IS CORRODED. (C-CHECK RO 1/26/2025) REMOVED AND REPLACED SERVICE DOOR SURROUND STRUCTURE LOWER SILL P/N 601R38533-9 IAW CRJ200 SRM 51-42-21 TASK CARD 51-900-1003-SKY COMPLETED. M-337 ATTACHED. CPCP MANUALLY EMA
- [SDR SWIA20250127006](https://openairdocs.org/sdr/SWIA20250127006.md): Skin · dented · Oct 6, 2024 · N679SA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > ADM# N679SA-8142THERE IS A DENT ABOVE AND AFT OF LOW PRESSURE AIR ACCESS PANEL, BETWEEN APPROXIMATELY FS589-FS605, AND STRINGER 21R-22R. PLEASE PLOT, MAP, AND EVALUATE DAMAGE. IF FOUND WITHIN LIMITS, ELIMINATE ALL EVIDENCE OF DAMAGE USING AIRCRAFT STANDARD PRA
- [SDR SWIA202306196001](https://openairdocs.org/sdr/SWIA202306196001.md): Unknown · warning message · Jun 16, 2023 · N679SA · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > FLAPS FAIL CAUTION MESSAGE ON APPROACH AT ATW WHEN SELECTING FLAPS. INDICATED ZERO DEGREES. FOLLOWED QRH. PREFORMED A NO FLAP LANDING AT ORD. (FLT 4742 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 26767675 WITH THE FOLLOWING CORRECTIVE ACTION: "R
- [SDR SWIA202301301](https://openairdocs.org/sdr/SWIA202301301.md): None · damaged · Jan 30, 2023 · N679SA · Cndair CL6002B19 · Wing Main, Frame Structure
  > FOUND LH WING WING BOX EXTENSION TRAILING EDGE ASSEMBLY DAMAGED (REF. IPC 57-32-00 ITEM #130) (FILED CLOSED)REMOVED AND REPLACED LH WING BOX EXTENSION TRAILING EDGE ASSEMBLY IN REFERENCE TO DWG. 600-10387 REV. D, SRM 51-21-00, SRM 51-40-11, SRM 51-41-00.ALL WO
- [SDR SWIA2022122967069](https://openairdocs.org/sdr/SWIA2022122967069.md): Bracket · cracked · Dec 6, 2022 · N679SA · Cndair CL6002B19 · Horizontal Stabilizer Structure
  > PANEL 326BR FWD NUT PLATE BRACKET CRACKED AT HORIZONTAL STABILIZER. REMOVED ANGLE VISOR SUPPORT IAW SRM 51-42-06. INSTALLED NEW ANGLE VISOR SUPPORT IAW SRM, 51-42-06 AND DWG 600-23060 REV-V.
- [SDR SWIA2022122967068](https://openairdocs.org/sdr/SWIA2022122967068.md): Skin · dented · Dec 4, 2022 · N679SA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT ON EXTERNAL FUSELAGE SKIN REPAIR DOUBLER BETWEEN FS 589.00 - 605.00, STGR 25R - 26R. PERFORMED REPAIR TO DENT ON EXTERNAL FUSELAGE SKIN REPAIR DOUBLER IAW REO 601R-53-61-7930 REV -.
- [SDR SWIA2022122967067](https://openairdocs.org/sdr/SWIA2022122967067.md): Skin · dented · Dec 4, 2022 · N679SA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT ON EXTERNAL FUSELAGE SKIN BETWEEN FS 640.00 - 654.00, STGR 19L - 20L. REPAIRED DENT IN FUSELAGE SKIN IAW REO 601R-53-61-7927 REV -.
- [SDR SWIA202266451](https://openairdocs.org/sdr/SWIA202266451.md): None · cracked · Sep 11, 2022 · N679SA · Cndair CL6002B19 · Window/Windshield System
  > CAPTAIN SIDE WINDSHIELD CRACKED DURING CRUISE (FLIGHT #5451 FILED CLOSED) PLEASE REFERENCE AML 992932 FOR NEW REPLACEMENT OF CAPTAINS WIPER ARM. R&R CAPTAINS SIDE WINDSHIELD IN REF TO AMM 56-11-01 AND MIP TASK CARD 56-220-1000-SKY. OPS CHECK AND LEAK C
- [SDR SWIA202265987](https://openairdocs.org/sdr/SWIA202265987.md): None · shutdown · Jul 7, 2022 · N679SA · Cndair CL6002B19 · Engine Oil Quantity
  > R ENG OIL PRESS WARNING MESSAGE NEAR TOP OF CLIMB PASSING THROUGH F300. R ENGINE OIL PRESSURE INDICATION FLUCTUATING INTO LOW RED PRESSURE ZONE. FOLLOWED QRH RETARDED ENGINE TO IDLE AND CONTINUED TO GET MESSAGE. FOLLOWED IN FLIGHT ENGINE SHUTDOWN PROCEDURE.
- [SDR SWIA202156964](https://openairdocs.org/sdr/SWIA202156964.md): Warning Message · false activation · Mar 17, 2021 · N679SA · Cndair CL6002B19 · Ice/Rain Protection System
  > ANTI-ICE WARNING MESSAGE IN FLIGHT SHORTLY AFTER TAKE OFF. FLIGHT 5491 NO HISTORY OF ANTI-ICE DUCT OR ANTI-ICE WARNING MSG. INSPECTED RIGHT WING FOR SIGNS OF BLEED LEAK. NO BLEED LEAK NOTED AT THIS TIME. PER FIM 36-20-00 SUSPECT FAULTY RIGHT BLCU. REMOVED A
- [SDR SWIA202053968](https://openairdocs.org/sdr/SWIA202053968.md): Spar · bent · Nov 9, 2020 · N679SA · Cndair CL6002B19 · Wing Spar
  > REAR SPAR (P/N 601R10851-3 SRM 57-21-07, FIG 4 ITEM 11) LOWER FLANGE BETWEEN WS 371.00-WS 377.00 IS BENT 0.200" UPWARD ALONG 2.20" SPANWISE. CLASSIFIED AS MAJOR REPAIR M-337 INITIATED. FILED CLOSED. REPAIR OF REAR SPAR LOWER FLANGE PERFORMED BY MHIRJ MRT PE
- [SDR SWIA202053967](https://openairdocs.org/sdr/SWIA202053967.md): Skin · bent · Nov 9, 2020 · N679SA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > LOWER SKIN (P/N 601R10871-3 SRM ITEM 8) BETWEEN WS 371.00 WS 377.00 IS BENT 0.250" UPWARD ALONG 3.50" SPANWISE & 1.00? CHORDWISE. CLASSIFIED AS MAJOR REPAIR M-337 INITIATED. FILED CLOSED. REPAIR OF LOWER SKIN PERFORMED BY MHIRJ MRT PERSONNEL, PER REO. COMP
- [SDR SWIA202053966](https://openairdocs.org/sdr/SWIA202053966.md): Strap · damaged · Nov 9, 2020 · N679SA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LOWER STRAP (P/N 601R10871-9 SRM 57-21-31, FIG 3 ITEM 11) WS 371.00-WS 377.00 IS HEAVILY BENT AND SHEARED. CLASSIFIED AS MAJOR REPAIR M-337 INITIATED. FILED CLOSED. NEW LOWER STRAP FABRICATED AND INSTALLED BY MHIRJ MRT PERSONNEL, PER REO, REFERENCE SNIEO FO
- [SDR SWIA202053468](https://openairdocs.org/sdr/SWIA202053468.md): Bracket · cracked · Oct 19, 2020 · N679SA · Cndair CL6002B19 · Cargo/Baggage Doors
  > FWD CARGO DOOR TRACK LOWER BRACKET CRACKED. FILED CLOSED. REPLACED FWD CARGO DOOR TRACK LOWER BRACKET, IN REFERENCE TO CRJ 200 SRM.
- [SDR SWIA2019110546713](https://openairdocs.org/sdr/SWIA2019110546713.md): Transmitter · out of tolerance · Nov 5, 2019 · N679SA · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > R/H WING FLAP POSITION TRANSMITTER OUT OF SYNC WITH L/H WING FLAP TRANSMITTER. (C-CHECK) RO: 11/04/2019 WORK PERFORMED BY VENDOR AVMAX,
- [SDR SWIA2019110546712](https://openairdocs.org/sdr/SWIA2019110546712.md): Panel · damaged · Nov 5, 2019 · N679SA · Cndair CL6002B19 · Vertical Stabilizer, Plate/Skin
  > PANEL 325AR HAS DAMAGE OUT OF SRM LIMITS. REQUIRES REO FOR RECTIFICATION, (PANEL OPENING LANDING). (C-CHECK) RO: 11/04/2019 WORK PERFORMED BY VENDOR AVMAX.
- [SDR SWIA2019110546711](https://openairdocs.org/sdr/SWIA2019110546711.md): Panel · damaged · Nov 5, 2019 · N679SA · Cndair CL6002B19 · Vertical Stabilizer, Plate/Skin
  > PANEL 325BL AND 325CL HAS DAMAGE OUT OF SRM LIMITS. REQUIRES REO FOR RECTIFICATION, (PANEL OPENING LANDING). (C-CHECK) RO: 11/04/2019 WORK PERFORMED BY VENDOR AVMAX. SEE ATTACHED WORK CARD FOR DETAILS.
- [SDR SWIA2019110546710](https://openairdocs.org/sdr/SWIA2019110546710.md): Control Cable · out of adjust · Nov 5, 2019 · N679SA · Cndair CL6002B19 · Elevator Control System
  > ELEVATOR AUTOPILOT CONTROL CABLE OUT OF TENSION LIMITS. (C-CHECK) RO: 11/04/2019 ADJUSTE AUTOPILOT CONTROL CABLES IAW AMM.
- [SDR SWIA2019110546709](https://openairdocs.org/sdr/SWIA2019110546709.md): Structure · dented · Nov 5, 2019 · N679SA · Cndair CL6002B19 · Spoilers
  > RH FLIGHT SPOILER HAS MANY DENTS AND IS OUT OF LIMITS PER SRM CUSTOMER HAS REQUESTED REMOVAL AND A NEW RH FLIGHT SPOILER INSTALLED. (C-CHECK) RO: 11/04/2019 REPLACED RH FLIGHTS SPOILER ASSY.
- [SDR SWIA2019110546708](https://openairdocs.org/sdr/SWIA2019110546708.md): Pump · leaking · Nov 5, 2019 · N679SA · Cndair CL6002B19 · Fuel Boost Pump
  > FUEL SEEPING OUT OF 5 EA. SCREW HOLES ON L/H ELECTRICAL BOOST PUMP. (C-CHECK) RO: 11/04/2019 RE-SEALED DOME NUTS. LEAK CHECKS GOOD.
- [SDR SWIA2019110546707](https://openairdocs.org/sdr/SWIA2019110546707.md): Throttle · out of adjust · Nov 5, 2019 · N679SA · Cndair CL6002B19 · Power Lever
  > LH THROTTLE OUT OF LIMITS AND HAS HIGH RESISTANCE WHEN MOVING. (C-CHECK) RO: 11/04/2019 PERFORMED ADJUSTMENT AND RIGGING CHECKS OF THROTTLES. OPS CHECKS GOOD.
- [SDR SWIA2019110546706](https://openairdocs.org/sdr/SWIA2019110546706.md): Potentiometer · out of tolerance · Nov 5, 2019 · N679SA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > POTENTIOMETER 5,6,7 AND 8 OUT OF TOLERANCE (READING.011) ON FECU. (C-CHECK) RO: 11/04/2019 WORK PERFORMED BY VENDOR AVMAX.
- [SDR SWIA2019110546705](https://openairdocs.org/sdr/SWIA2019110546705.md): Flap · out of tolerance · Nov 5, 2019 · N679SA · Cndair CL6002B19 · Trailing Edge Flaps
  > RH O/B FLAP POP MARKS OUT OF TOLERANCE. (C-CHECK) RO: 11/04/2019 WORK PERFORMED BY VENDOR AVMAX,
- [SDR SWIA2019110546704](https://openairdocs.org/sdr/SWIA2019110546704.md): Potentiometer · out of tolerance · Nov 5, 2019 · N679SA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > RH BPSU POTENTIOMETER OUT OF TOLERANCE. (C-CHECK) RO: 11/04/2019 WORK PERFORMED BY VENDOR AVMAX,
- [SDR SWIA2019110546703](https://openairdocs.org/sdr/SWIA2019110546703.md): Potentiometer · out of tolerance · Nov 5, 2019 · N679SA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > LH BPSU POTENTIOMETER OUT OF TOLERAANCE. (C-CHECK) RO: 11/04/2019 WORK PERFORMED BY VENDOR AVMAX.
- [SDR SWIA2019110546702](https://openairdocs.org/sdr/SWIA2019110546702.md): Support Beam · corroded · Nov 5, 2019 · N679SA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT BEAM AT FS 409+70, ON LBL 9 INBVOARD FLANGE AT FLOOR BOARD NUT PLATE HOLE HAS CORROSION. (C-CHECK) RO: 11/04/2019 PERFORMED REPAIR TO FLOOR SUPPORT BEAM AT FS 409+70 LBL 9. COMPLIED WITH FORM M-337.
- [SDR SWIA2019110546701](https://openairdocs.org/sdr/SWIA2019110546701.md): Fitting · corroded · Nov 5, 2019 · N679SA · Cndair CL6002B19 · Ailerons
  > O/B LUG ON O/B PCU FITTING ON RH AILERON HAS CORROSION. (C-CHECK) RO: 11/04/2019 REMOVED CORROSION BY OVERSIZING RH AILERON, OUTBOARD PCU LUG. COMPLIED WITH M-337.
- [SDR SWIA2019110546700](https://openairdocs.org/sdr/SWIA2019110546700.md): Fitting · cracked · Nov 5, 2019 · N679SA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RH WINDOW SIDE POST - LOWER AFT FITTING (CLIP) CRACKED. (C-CHECK) RO: 11/04/2019 REPLACED RH WINDOW SIDE POST LOWER AFT FITTING. COMPLIED WITH M-337.
- [SDR SWIA2019110546699](https://openairdocs.org/sdr/SWIA2019110546699.md): Fitting · cracked · Nov 5, 2019 · N679SA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LH WINDOW SIDE POST - LOWER AFT FITTING (CLIP) CRACKED. (C-CHECK) RO: 11/04/2019 REPLACE LH WINDOW SIDE POST, LOWER AFT FITTING. COMPLIED WITH M-337.
- [SDR SWIA2019110546698](https://openairdocs.org/sdr/SWIA2019110546698.md): Support Beam · corroded · Nov 5, 2019 · N679SA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > VERTICAL FLOOR SUPPORT BEAM AT RBL27 FS 409+128 IS CRACKED AT LOWER INBOARD AFT CORNER. (C-CHECK) RO: 11/04/2019 PERFORMED CUTOUT REPAIR TO VERTICAL FLOOR SUPPORT BEAM AT RBL 27 FS 409+128. COMPLIED WITH M-337.
- [SDR SWIA2019110546697](https://openairdocs.org/sdr/SWIA2019110546697.md): Support Beam · cracked · Nov 5, 2019 · N679SA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > VERTICAL FLOOR SUPPORT BEAM AT LBL27 FS 409 +128 IS CRACKED AT LOWER INBOARD AFT CORNER. (C-CHECK) RO: 11/04/2019 PERFORMED REPAIR TO FLOOR SUPPORT BEAM LBL 27 FS 409+128. COMPLIED WITH M-337.
- [SDR SWIA2019110546696](https://openairdocs.org/sdr/SWIA2019110546696.md): Structure · cracked · Nov 5, 2019 · N679SA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR FRAME AT FS280 IS CRACKED IN 2 SPOTS RBL9 AND LBL12. (C-CHECK) RO: 11/04/2019 WORK PERFORMED BY VENDOR AVMAX. COMPLIED WITH M-337.
- [SDR SWIA2019110546689](https://openairdocs.org/sdr/SWIA2019110546689.md): Doubler · corroded · Nov 5, 2019 · N679SA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CABIN - PRESS FLOOR DOUBLER AND WEB CORROSION FS424 - 439 RBL38 - 42. (C-CHECK) RO: 11/04/2019 BLENDED OUT CORROSION TO PRESSURE FLOOR PANEL. COMPLIED WITH M-337.
- [SDR SWIA2019110546679](https://openairdocs.org/sdr/SWIA2019110546679.md): Floor Panel · corroded · Nov 5, 2019 · N679SA · Cndair CL6002B19 · Fuselage Floor Panel
  > CABIN - PRESSURE FLOOR CORROSION. FS424 - 439, LBL38-42. (C-CHECK) RO: 11/04/2019 BLENDED OUT CORROSION TO PRESSURE FLOOR PANEL. COMPLIED WITH M-337.
- [SDR SWIA2019110546677](https://openairdocs.org/sdr/SWIA2019110546677.md): Door Sill · corroded · Nov 5, 2019 · N679SA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CABIN - PRESSURE FLOOR - WEB & DOUBLER CORRODED FS439-449 RBL38-42. (C-CHECK) RO: 11/04/2019 BLENDED OUT CORROSION ON PRESSURE FLOOR SILL PANEL AND ANGLE. BLENDS WITHIN LIMITS. COMPLIED WITH M-337.
- [SDR SWIA2019110546676](https://openairdocs.org/sdr/SWIA2019110546676.md): Frame · chafed · Nov 5, 2019 · N679SA · Cndair CL6002B19 · Fuselage Main, Frame
  > CHAFE DAMAGE AT AFT EDGE OF RH FRAME AT FS559+48 BETWEEN STR2R AND STR3R. (C-CHECK) RO: 11/04/2019 PERFORMED REPAIR TO FRAME DAMAGE AT FS 559+48 BETWEEN STR 2R AND 3R. COMPLIED WITH M-337.
- [SDR SWIA2019110546675](https://openairdocs.org/sdr/SWIA2019110546675.md): Door Sill · corroded · Nov 5, 2019 · N679SA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON RH OTBD FLOOR SILL BETWEEN FS559 AND FS559+32. (C-CHECK) RO: 11/04/2019 REPLACED FLOOR SILL AT FS 559-559+16 TO 559+32. COMPLIED WITH M-337.
- [SDR SWIA2019110546674](https://openairdocs.org/sdr/SWIA2019110546674.md): Support Fitting · damaged · Nov 5, 2019 · N679SA · Cndair CL6002B19 · Elevator Miscellaneous Structure
  > MECHANICAL DAMAGE ON THE INTERNAL FACE OF THE BACKUP FITTING FOR THE I/B HINGE FITTING ES14.47 FOR THE L/H ELEVATOR. (C-CHECK) RO: 11/04/2019 REPLACED SUPPORT FITTING AT ES 14.47. COMPLIED WITH M-337.
- [SDR SWIA2019110546673](https://openairdocs.org/sdr/SWIA2019110546673.md): Attach Fitting · corroded · Nov 5, 2019 · N679SA · Cndair CL6002B19 · Ailerons
  > CORROSION IN THE BORE AND BADLY WORN BUSHING AT THE OTBD LUG OF THE LH AILERON INBD PCU ATTACH FITTING. RADIAL CHAFE ON THE OTBD FACE. (C-CHECK) RO: 11/04/2019 REMOVED CORROSION FROM BORE OF LH AILERON I/B PCU FITTING BY OVERSIZING. COMPLIED WITH M-337.
- [SDR SWIA2019110546672](https://openairdocs.org/sdr/SWIA2019110546672.md): Fitting · corroded · Nov 5, 2019 · N679SA · Cndair CL6002B19 · Ailerons
  > PCU FITTING ON R/H AILERON HAS CORROSION AROUND THE INNER BUSHINGS. (C-CHECK) RO: 11/04/2019 REMOVED CORROSION ON RH AILERON PCU FITTINGS BY REAMING LUGS. COMPLIED WITH M-337.
- [SDR SWIA2019110546671](https://openairdocs.org/sdr/SWIA2019110546671.md): Spar · damaged · Nov 5, 2019 · N679SA · Cndair CL6002B19 · Trailing Edge Flaps
  > DAMAGED SPAR, LH IB FLAP BETWEEN WS 58.505 TO WS 61.506. (C-CHECK) RO: 11/04/2019 REPLACED DAMAGED SPAR/INTERCOSTAL. COMPLIED WITH M-337.
- [SDR SWIA2019110546670](https://openairdocs.org/sdr/SWIA2019110546670.md): Rib · damaged · Nov 5, 2019 · N679SA · Cndair CL6002B19 · Trailing Edge Flaps
  > DAMAGED RIB LH IB FLAP AT WS 91.338. (C-CHECK) RO: 11/04/2019 REPLACED DAMAGED RIB INSIDE LH I/B FLAP. COMPLIED WITH M-337.
- [SDR SWIA2019110546669](https://openairdocs.org/sdr/SWIA2019110546669.md): Intercostal · corroded · Nov 5, 2019 · N679SA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR CUT-OUT AREA-AFT FRAME FS 349.00 TO FS364.00, WL84.206 CORRODED INTERCOSTAL (FWD) FLAGGED. (C-CHECK) RO: 11/04/2019 PERFORMED REPAIR TO PAX DOOR INTERCOSTAL AT FS 349-364 WL 84.206. COMPLIED WITH M-337.
- [SDR SWIA2019110546668](https://openairdocs.org/sdr/SWIA2019110546668.md): Pump · damaged · Nov 5, 2019 · N679SA · Cndair CL6002B19 · Fuel Boost Pump
  > L/H BOOST PUMP 4 EA. FLAW INDICATIONS EMITTING FROM SATELLITE HOLES. (C-CHECK) RO: 11/04/2019 COMPLIED WITH CARD 51-900-1003-SKY AND FORM M-337
- [SDR SWIA201946667](https://openairdocs.org/sdr/SWIA201946667.md): Bulkhead · gouged · Nov 5, 2019 · N679SA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD WEB GOUGED W.L. 108, RBL 18.00. (C-CHECK) RO: 11/04/2019 ACCOMPLISHED BY VENDOR AVMAX

Next page: https://openairdocs.org/aircraft/N679SA/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N679SA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N679SA/reports

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